The first major structural component failure of a composite part on a commercial airplane occurred during the crash of American Airlines Flight 587. The fractured composite lugs that attached the vertical stabilizer to the aircraft tail and the fractured composite honeycomb rudder were examined as part of the National Transportation Safety Board investigation of the accident. In this paper the composite fractures are described and the resulting clues to the failure events are discussed.


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    Titel :

    Fractographic Examination of the Vertical Stabilizer and Rudder from American Airlines Flight 587


    Beteiligte:
    M. R. Fox (Autor:in) / C. R. Schultheisz (Autor:in) / J. R. Reeder (Autor:in)

    Erscheinungsdatum :

    2005


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fractographic Examination of the Vertical Stabilizer and Rudder from American Airlines Flight 587

    Fox, Matthew R. / Schultheisz, Carl R. / Reeder, James R. | NTRS | 2005



    Materials Examination of the Vertical Stabilizer from American Airlines Flight 587

    M. R. Fox / C. R. Schultheisz / J. R. Reeder et al. | NTIS | 2005


    Materials Examination of the Vertical Stabilizer from American Airlines Flight 587

    Fox, Matthew R. / Schultheisz, Carl R. / Reeder, James R. et al. | NTRS | 2005


    NASA Langley Inspection of Rudder and Composite Tail of American Airlines Flight 587

    Winfree, William / Madaras, Eric / Cramer, K. et al. | AIAA | 2005